MIL-DTL-81969/39B
TABLE I. Metric equivalents.
Inches
mm
Inches
mm
Inches
mm
Inches
mm
.0075
.190
.072
1.83
.170
4.32
.280
7.11
.0085
.216
.075
1.90
.180
4.57
.290
7.37
.020
.51
.085
2.16
.190
4.83
.480
12.19
.026
.66
.095
2.41
.195
4.95
.520
13.21
.028
.71
.105
2.67
.200
5.08
1.180
29.97
.040
1.02
.126
3.20
.203
5.16
1.230
31.24
.068
1.73
.140
3.56
.250
6.35
2.010
51.15
.069
1.75
.146
3.71
.260
6.60
2.053
52.15
.071
1.80
.147
3.73
.270
6.86
4.24
107.7
NOTES:
1. Dimensions are in inches.
2. Metric equivalents are given for general information only and based upon
1.00 inch = 25.4 mm.
3. Unless otherwise specified, tolerances are +/-.005 (.13 mm) and +/-2 degrees for angles.
4. Plastic tips are capable of being separated from center section.
5. When testing thrust, the axial load applied should be 3 lb. for the insertion side and 10 lb. for
the removal side.
FIGURE 1. Installing and removal tool - continued.
REQUIREMENTS:
1. Dimensions and configuration: See figure 1.
2. Material: Acetal homopolymer or equivalent.
3. Finish: Installing tip green, removal tip white.
4. Plating: Not applicable.
5. Plunger force: Not applicable.
6. Plastic tips shall be smooth and free of burrs and sharp edges.
2
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